CA2465163C - Dispositif et methodes d'actionnement d'elements rotatifs - Google Patents
Dispositif et methodes d'actionnement d'elements rotatifs Download PDFInfo
- Publication number
- CA2465163C CA2465163C CA002465163A CA2465163A CA2465163C CA 2465163 C CA2465163 C CA 2465163C CA 002465163 A CA002465163 A CA 002465163A CA 2465163 A CA2465163 A CA 2465163A CA 2465163 C CA2465163 C CA 2465163C
- Authority
- CA
- Canada
- Prior art keywords
- actuator
- drive member
- coupled
- assembly
- extendible
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000000034 method Methods 0.000 title claims abstract description 23
- 238000006243 chemical reaction Methods 0.000 claims abstract description 111
- 238000004873 anchoring Methods 0.000 claims abstract description 10
- 241000272517 Anseriformes Species 0.000 claims description 60
- 230000000712 assembly Effects 0.000 claims description 6
- 238000000429 assembly Methods 0.000 claims description 6
- 230000008878 coupling Effects 0.000 claims description 2
- 238000010168 coupling process Methods 0.000 claims description 2
- 238000005859 coupling reaction Methods 0.000 claims description 2
- 230000008901 benefit Effects 0.000 description 15
- 230000007935 neutral effect Effects 0.000 description 4
- 238000005452 bending Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000004308 accommodation Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/04—Noseplanes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/12—Canard-type aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/10—Stabilising surfaces adjustable
- B64C5/16—Stabilising surfaces adjustable about spanwise axes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/02—Mounting or supporting thereof
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
Abstract
Un appareil et des méthodes pour actionner des éléments orientables sont décrits. Dans une réalisation, un ensemble pour actionner un élément orientable inclut un dispositif d'actionnement extensible comportant deux extrémités, et un organe d'entraînement doté d'une première partie couplée sur pivot à la seconde extrémité, et une seconde partie non couplée sur pivot à l'élément orientable. La seconde partie de l'organe d'entraînement est espacée par rapport à la première partie. L'organe d'entraînement inclut en outre une troisième partie espacée par rapport à la première et à la seconde partie dans une orientation non linéaire. L'assemblage inclut en outre une liaison de réaction dotée d'une extrémité d'ancrage couplée sur pivot à la première extrémité d'un dispositif d'actionnement extensible et une extrémité d'entraînement couplée sur pivot à la troisième partie de l'organe d'entraînement.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/426,400 US6698688B1 (en) | 2002-10-22 | 2003-04-29 | Apparatus and methods for actuating rotatable members |
US10/426,400 | 2003-04-29 |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2465163A1 CA2465163A1 (fr) | 2004-10-29 |
CA2465163C true CA2465163C (fr) | 2008-09-02 |
Family
ID=32990404
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA002465163A Expired - Lifetime CA2465163C (fr) | 2003-04-29 | 2004-04-23 | Dispositif et methodes d'actionnement d'elements rotatifs |
Country Status (6)
Country | Link |
---|---|
EP (1) | EP1473223B1 (fr) |
JP (1) | JP4646543B2 (fr) |
BR (1) | BRPI0402700A (fr) |
CA (1) | CA2465163C (fr) |
DE (1) | DE602004011139D1 (fr) |
RU (1) | RU2353545C2 (fr) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP5514527B2 (ja) * | 2009-12-11 | 2014-06-04 | ナブテスコ株式会社 | 航空機用リアクションリンク |
JP5552340B2 (ja) | 2010-03-15 | 2014-07-16 | ナブテスコ株式会社 | アクチュエータ及びリンクの製造方法、アクチュエータ及びリンクの設計方法、アクチュエータ及びリンク |
JP6383901B1 (ja) * | 2017-08-31 | 2018-08-29 | 一夫 有▲吉▼ | 横ひれ付き省エネジエット機 |
CN112173073B (zh) * | 2020-09-25 | 2023-05-26 | 中国直升机设计研究所 | 一种单舵机控制双垂尾操纵结构 |
CN113212734B (zh) * | 2021-06-20 | 2023-02-14 | 西北工业大学 | 一种小体积轻量化的机翼前缘缝翼作动机构 |
CN117973151B (zh) * | 2024-03-27 | 2024-05-31 | 北京航空航天大学 | 一种压电层合板壳结构振动控制方法、***及设备 |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3874617A (en) * | 1974-07-17 | 1975-04-01 | Mc Donnell Douglas Corp | Stol flaps |
US4043523A (en) * | 1976-03-11 | 1977-08-23 | Ball Brothers Research Corporation | Apparatus for aircraft pitch trim |
JPS5973395A (ja) * | 1982-10-20 | 1984-04-25 | 三菱重工業株式会社 | カナ−ド付き航空機 |
JPH0676801B2 (ja) * | 1986-01-10 | 1994-09-28 | 三菱重工業株式会社 | 油圧駆動機構のトリム操作装置 |
JPH0597095A (ja) * | 1991-10-09 | 1993-04-20 | Mitsubishi Heavy Ind Ltd | 航空機用非常操舵システム |
JPH05155389A (ja) * | 1991-12-03 | 1993-06-22 | Mitsubishi Heavy Ind Ltd | カナード翼 |
US5388788A (en) * | 1993-12-16 | 1995-02-14 | The Boeing Company | Hinge fairings for control surfaces |
FR2719548B1 (fr) * | 1994-05-03 | 1996-07-05 | Aerospatiale | Avion de transport à empennage avant. |
-
2004
- 2004-04-23 CA CA002465163A patent/CA2465163C/fr not_active Expired - Lifetime
- 2004-04-28 JP JP2004133508A patent/JP4646543B2/ja not_active Expired - Lifetime
- 2004-04-28 EP EP04076261A patent/EP1473223B1/fr not_active Expired - Lifetime
- 2004-04-28 DE DE602004011139T patent/DE602004011139D1/de not_active Expired - Lifetime
- 2004-04-28 RU RU2004113258/11A patent/RU2353545C2/ru active
- 2004-04-29 BR BR0402700-0A patent/BRPI0402700A/pt not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
DE602004011139D1 (de) | 2008-02-21 |
CA2465163A1 (fr) | 2004-10-29 |
EP1473223A1 (fr) | 2004-11-03 |
RU2004113258A (ru) | 2005-10-20 |
JP4646543B2 (ja) | 2011-03-09 |
EP1473223B1 (fr) | 2008-01-09 |
BRPI0402700A (pt) | 2004-11-30 |
JP2004323012A (ja) | 2004-11-18 |
RU2353545C2 (ru) | 2009-04-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request | ||
MKEX | Expiry |
Effective date: 20240423 |